View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 22823U 26150.13316420 +.00000000 +00000-0 +99547-4 0 00002
2 22823 98.8576 214.1382 0015660 296.1093 63.8472 14.20088442 04
| Epoch (UTC): | 30 May 2026 03:11:45 |
| Eccentricity: | 0.0015660 |
| inclination: | 98.8576° |
| perigee height: | 814 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 214.1382° |
| argument of perigee: | 296.1093° |
| revolutions per day: | 14.20088442 |
| mean anomaly at epoch: | 63.8472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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